KR20160138176A - A polymer composition, an article thereof and a process for preparing the same - Google Patents

A polymer composition, an article thereof and a process for preparing the same Download PDF

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KR20160138176A
KR20160138176A KR1020167029377A KR20167029377A KR20160138176A KR 20160138176 A KR20160138176 A KR 20160138176A KR 1020167029377 A KR1020167029377 A KR 1020167029377A KR 20167029377 A KR20167029377 A KR 20167029377A KR 20160138176 A KR20160138176 A KR 20160138176A
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weight
composition
polyamide
laser
thermoplastic
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KR1020167029377A
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Korean (ko)
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렌 바오
로버트 헨드릭 카타리나 얀센
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디에스엠 아이피 어셋츠 비.브이.
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Publication of KR20160138176A publication Critical patent/KR20160138176A/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B7/00Mixing; Kneading
    • B29B7/30Mixing; Kneading continuous, with mechanical mixing or kneading devices
    • B29B7/34Mixing; Kneading continuous, with mechanical mixing or kneading devices with movable mixing or kneading devices
    • B29B7/38Mixing; Kneading continuous, with mechanical mixing or kneading devices with movable mixing or kneading devices rotary
    • B29B7/46Mixing; Kneading continuous, with mechanical mixing or kneading devices with movable mixing or kneading devices rotary with more than one shaft
    • B29B7/48Mixing; Kneading continuous, with mechanical mixing or kneading devices with movable mixing or kneading devices rotary with more than one shaft with intermeshing devices, e.g. screws
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29B7/00Mixing; Kneading
    • B29B7/80Component parts, details or accessories; Auxiliary operations
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • BPERFORMING OPERATIONS; TRANSPORTING
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    • C23C18/00Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
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    • C23C18/00Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
    • C23C18/16Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
    • C23C18/18Pretreatment of the material to be coated
    • C23C18/20Pretreatment of the material to be coated of organic surfaces, e.g. resins
    • C23C18/2006Pretreatment of the material to be coated of organic surfaces, e.g. resins by other methods than those of C23C18/22 - C23C18/30
    • C23C18/2026Pretreatment of the material to be coated of organic surfaces, e.g. resins by other methods than those of C23C18/22 - C23C18/30 by radiant energy
    • C23C18/204Radiation, e.g. UV, laser
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    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C18/00Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
    • C23C18/16Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
    • C23C18/31Coating with metals
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    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
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    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
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    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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Abstract

본원은
a) 42.5 중량% 내지 94 중량%의 열가소성 매트릭스 수지;
b) 1 중량% 내지 7.5 중량%의 레이저 직접 구조화 첨가제; 및
c) 5 중량% 내지 50 중량%의 섬유 보강제
를 포함하고 레이저를 사용하여 활성화된 후 도금될 수 있는 열가소성 조성물로서,
상기 중량%는 조성물의 총 중량을 기준으로 하고;
상기 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서, x는 0.60 초과 및 0.85 미만인, 열가소성 조성물을 개시한다.
Here,
a) from 42.5% to 94% by weight of a thermoplastic matrix resin;
b) from 1% to 7.5% by weight of a laser direct structured additive; And
c) 5% to 50% by weight of fiber reinforcement
A thermoplastic composition that can be activated after laser activation,
Said weight percent being based on the total weight of the composition;
Wherein the laser direct structured additive is a thermoplastic composition represented by the formula Zn x Ni (1-x) Fe 2 O 4 , wherein x is greater than 0.60 and less than 0.85.

Description

중합체 조성물, 이의 제품 및 이의 제조 방법{A POLYMER COMPOSITION, AN ARTICLE THEREOF AND A PROCESS FOR PREPARING THE SAME}[0001] POLYMER COMPOSITION, PRODUCTS OF THE SAME, AND PROCESS FOR PRODUCING THE SAME [0002]

본원은 레이저 직접 구조화(Laser Direct Structuring: LDS) 첨가제를 포함하는 열가소성 중합체 조성물에 관한 것이다. 특히, 본 발명은 LDS 방법에 의해 제조된 제품 및 이의 제조 방법에 관한 것이다.The present invention relates to a thermoplastic polymer composition comprising a laser direct structuring (LDS) additive. In particular, the present invention relates to a product made by the LDS method and a method of making the same.

레이저 직접 구조화(LDS)는, 금속으로 선택적으로 도금하여 사출 성형된 제품을 별도의 전도성 회로 경로를 형성할 수 있는 방법이다. 먼저, 플라스틱 물품은 이 방법을 위해 특이적으로 제형화된 중합체 화합물을 사용하여 사출 성형된다. 이어서, 상기 물품은 목적한 패턴의 레이저로 활성화됨으로써 레이저를 사용하여 기술된 부분에서 물품을 표면을 활성화시킨다. 이어서, 상기 물품은 구리, 니켈 또는 금과 같은 금속으로 무전해 도금 공정을 거치고 생성된 회로 경로는 레이터 패턴에 정확히 부합한다. Laser direct structuring (LDS) is a method that can form a separate conductive circuit path by selectively plating metal and injection molded products. First, plastic articles are injection molded using polymeric compounds specifically formulated for this process. The article is then activated with a laser of the desired pattern, thereby activating the surface of the article at the portion described using the laser. The article is then subjected to an electroless plating process with a metal such as copper, nickel, or gold, and the resulting circuit path exactly matches the lator pattern.

레이저 직접 구조화(LDS) 방법의 장점은 사출 성형 물품의 윤곽을 따라 회로 경로를 가짐으로써 실제 3D 회로 경로를 적용하는 능력이다. 회로를 플라스틱 물품상에 직접 통합시킴으로써, 디자이너는 이제 이전에 사용할 수 없는 자유를 갖는다. 이러한 디자인 자유는 물품 강화(consolidation), 중량 감량, 소형화, 감소된 조립 시간, 개선된 신뢰도 및 전체 시스템 비용 감소를 허용한다.The advantage of the Laser Direct Structured (LDS) method is the ability to apply the actual 3D circuit path by having circuit paths along the contours of the injection molded article. By integrating the circuit directly onto the plastic article, the designer now has the freedom that was previously unavailable. This freedom of design allows for consolidation, weight reduction, miniaturization, reduced assembly time, improved reliability and reduced overall system cost.

레이저 직접 구조화 방법을 위한 주요 시장 및 적용은 의료, 자동차, 항공우주, 군대, 무선주파수(RF) 안테나, 센서, 주택 보안 및 커넥터를 포함한다.Key markets and applications for laser direct structured methods include medical, automotive, aerospace, military, radio frequency (RF) antennas, sensors, home security and connectors.

US 2009/0292051[(사빅:SABIC)]은 레이저 직접 구조화 방법에 사용될 수 있는 고유전 상수 열가소성 조성물을 개시한다. 상기 조성물은 열가소성 기재 수지, 레이저 직접 구조화 첨가제, 및 1종 이상의 세라믹 충전제를 포함한다. 열가소성 조성물은 하기를 포함하고, 레이저를 사용하여 활성화된 후 도금될 수 있다:US 2009/0292051 (SABIC: SABIC) discloses a high dielectric constant thermoplastic composition that can be used in a laser direct structuring method. The composition comprises a thermoplastic base resin, a laser direct structured additive, and at least one ceramic filler. The thermoplastic composition can be plated after activation using a laser, including:

a) 10 내지 90 중량%의 열가소성 기재 수지;a) from 10 to 90% by weight of a thermoplastic base resin;

b) 0.1 내지 30 중량%의 레이저 직접 구조화 첨가제; 및b) from 0.1 to 30% by weight of a laser direct structured additive; And

c) 10 내지 80 중량% 이하의 하나 이상의 세라믹 충전제.c) from 10 to 80% by weight of one or more ceramic fillers.

조성물은 고유전 상수, 저손실 탄젠트 열가소성 조성물을 제공한다. 구리 크로뮴 옥사이드 스피넬은 직접 구조화 첨가제로서 사용된다.The composition provides a high dielectric constant, low loss tangent thermoplastic composition. Copper chromium oxide spinel is used as a direct structured additive.

US 2012/0279764(SABIC)는 레이저 직접 구조화 방법에 사용되어 강화된 도금 성능 및 우수한 기계적 특성을 제공할 수 있는 열가소성 조성물을 개시한다. 상기 특허의 조성물은 열가소성 기재 수지, 레이저 직접 구조화 첨가제 및 백색 안료를 포함한다. US 2012/0279764 (SABIC) discloses thermoplastic compositions that can be used in laser direct structuring methods to provide enhanced plating performance and excellent mechanical properties. The composition of the patent includes a thermoplastic base resin, a laser direct structured additive and a white pigment.

열가소성 조성물은,The thermoplastic composition may comprise,

a) 65 내지 92 중량%의 열가소성 기재 수지;a) 65 to 92% by weight of a thermoplastic base resin;

b) 0.5 내지 20 중량%의 레이저 직접 구조화 첨가제; 및b) from 0.5 to 20% by weight of a laser direct structured additive; And

c) 0.5 내지 15 중량%의, 아나티즈, 루틸, 코팅되고 코팅되지 않은 ZnO, BaSO4, CaCO3, BaTiO3 또는 상기한 안료 중 하나 이상을 포함하는 조합을 포함하는 TiO2로부터 선택된 하나 이상의 안료c) from 0.5 to 15% by weight of one or more pigments selected from TiO 2 comprising a combination comprising at least one of the following: anatase, rutile, uncoated ZnO, BaSO 4 , CaCO 3 , BaTiO 3 ,

를 포함하고 레이저를 사용하여 활성화된 후 도금될 수 있고,Lt; / RTI > and may be activated using a laser and then plated,

상기 레이저 직접 구조화 첨가제는 중금속 혼합물 옥사이드 스피넬, 예컨대 구리 크로뮴 옥사이드 스피넬; 구리 염, 예컨대 구리 하이드록사이드, 구리 포스페이트, 구리 설페이트, 제 1 구리 티오시아네이트; 또는 상기한 레이저 직접 구조화 첨가제 중 하나 이상을 포함하는 조합이다.The laser direct structured additive may be a heavy metal mixture oxide spinel, such as copper chromium oxide spinel; Copper salts such as copper hydroxide, copper phosphate, copper sulfate, cuprous thiocyanate; Or a laser direct structured additive as described above.

US 2004/0241422(LPKF)는, 지지 물질에 분산된 전기적 비전도성 금속 화합물을 분해하기 위해 전자기 방사선을 사용하여 생성된 금속 핵 상에 금속화된 층을 증착시킴으로써 전기적 비전도성 지지 물질상에 배치된 전도성 트랙을 생성하는 방법, 및 이를 생성하는 방법을 개시한다. 전기적 비전도성 금속 화합물은, 열에 안정하고 산성 또는 알칼리 금소화 욕에서 안정하고, 열에 안정하고 산성 또는 알칼리 금소화 욕에서 안정한 고급 옥사이드이고, 스피넬 구조를 갖는 고급 옥사이드이고, 비-조사 영역에서 불변인 채로 남아 있는, 불용성 스피넬계 무기 옥사이드이다. 사용된 스피넬계 무기 옥사이드는 내열성이고 납땜 온도를 겪은 후 안정한 채로 있다. 전도체 트랙은 견실하고 용이하게 생성되고 지지체에 강하게 부착된다.US 2004/0241422 (LPKF) discloses a method of depositing a metal layer on an electrically nonconductive support material by depositing a metallized layer on the metal nuclei produced using electromagnetic radiation to decompose the electrically nonconductive metal compound dispersed in the support material A method of generating a conductive track, and a method of generating it, are disclosed. The electrically nonconductive metal compound is a high-grade oxide which is stable in heat, stable in an acidic or alkaline digesting bath, stable in heat and stable in an acidic or alkaline digesting bath, is an oxide having a spinel structure, Insoluble spinel-based inorganic oxide. The spinel-based inorganic oxide used is heat-resistant and remains stable after experiencing the soldering temperature. The conductor tracks are robust and easily produced and strongly attached to the support.

US 2008/0015320[뒤퐁(DU-PONT)]은 중합체 조성물의 총 중량의 40, 45, 50, 55, 60, 65, 70, 75, 80, 85, 90, 95, 96 또는 97 중량%의 양으로 존재하는 중합체 결합제; 중합체 조성물의 총 중량의 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 20, 25, 30, 35, 40, 45, 50, 55 및 60 중량%의 양으로 존재하는 스피넬 결정 충전제를 포함하는 광-활성가능한 중합체 조성물, 및 이의 제조 방법을 개시한다. 상기 문헌의 실시예에서, CuCr2O4가 스피넬로서 사용된다.US 2008/0015320 (DU-PONT) discloses a process for the preparation of a polymer composition which comprises adding to the polymer composition a quantity of 40, 45, 50, 55, 60, 65, 70, 75, 80, 85, 90, 95, 96 or 97% ≪ / RTI > The total weight of the polymer composition was determined to be 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 20, 25, 30, 35, 40, 45, %, Based on the total weight of the composition, of a spinel crystal filler, and a process for producing the same. In the examples of this document, CuCr 2 O 4 is used as the spinel.

LPKF 기술에 기초한 종래 기술에서, CuCr2O4 스피넬은 레이저 직접 구조화 방법에 사용되는 매트릭스 수지를 사용할 수 있는 레이저 직접 구조화 첨가제로서 사용된다. LDS 첨가제로서 CuCr2O4 스피넬을 사용하는 한가지 단점은, CuCr2O4 스피넬이 매트릭스 중합체의 기계적 특성에 유해하다는 점이다. 따라서, 생성된 중합체의 적용은 제한될 것이다. 반면에, NiFe2O4와 같은 스피넬은 전혀 도금될 수 없고 또한 기계적 특성에 좋지 않음을 관찰하였다. 본원에서, CuCr2O4는 또 다른 첨가제 Ni-Zn 페라이트(ZnFe2O4로 도핑된 NiFe2O4)로 대체되어 레이저를 사용하여 활성화된 후 도금될 수 있는 열가소성 중합체 조성물을 수득하였다. LDS 첨가제로서 CuCr2O4 스피넬을 사용하는 조성물과 비교하여, 본원의 생성된 조성물의 기계적 특성은 개선된다. In the prior art based on LPKF technology, CuCr 2 O 4 spinel is used as a laser direct structured additive which can use matrix resins used in laser direct structuring methods. One drawback of using a CuCr 2 O 4 spinel as the LDS additive is that the CuCr 2 O 4 spinel that harmful to the mechanical properties of the matrix polymer. Therefore, the application of the resulting polymer will be limited. On the other hand, it has been observed that spinel such as NiFe 2 O 4 can not be plated at all and is poor in mechanical properties. Herein, CuCr 2 O 4 is to give the thermoplastic polymer composition, which addition is replaced by the other additives, Ni-Zn ferrite (ZnFe 2 O 4 with NiFe 2 O 4 doped with) may be plated after being activated using a laser. Compared to compositions using CuCr 2 O 4 spinel as an LDS additive, the mechanical properties of the resulting compositions herein are improved.

본원은Here,

a) 42.5 중량% 내지 94 중량%의 열가소성 매트릭스 수지;a) from 42.5% to 94% by weight of a thermoplastic matrix resin;

b) 1 중량% 내지 7.5 중량%의 레이저 직접 구조화 첨가제; 및b) from 1% to 7.5% by weight of a laser direct structured additive; And

c) 5 중량% 내지 50 중량%의 섬유 보강제c) 5% to 50% by weight of fiber reinforcement

를 포함하고 레이저에 의해 활성화된 후 도금될 수 있는 열가소성 중합체 조성물로서;≪ / RTI > and can be plated after being activated by a laser;

상기 중량%는 조성물의 충 중량을 기준으로 하고;Said weight percent being based on the fill weight of the composition;

상기 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서, x는 0.60 초과 및 0.85 미만인, 열가소성 중합체 조성물을 제공한다.Wherein the laser direct structured additive is a thermoplastic polymer composition represented by the formula Zn x Ni (1-x) Fe 2 O 4 , where x is greater than 0.60 and less than 0.85.

열가소성 매트릭스 수지는 폴리에스터, 폴리아미드, 폴리페닐렌 설파이드, 폴리페닐렌 옥사이드, 폴리설폰, 폴리아릴레이트, 폴리에테르에테르케톤, 폴리에테르이미드, 및 이의 혼합물 및/또는 공중합체로 이루어진 군으로부터 하나 이상 선택될 수 있다. The thermoplastic matrix resin may comprise one or more compounds selected from the group consisting of polyesters, polyamides, polyphenylene sulfides, polyphenylene oxides, polysulfones, polyarylates, polyetheretherketones, polyetherimides, and mixtures and / Can be selected.

바람직하게는, 열가소성 매트릭스 수지는 폴리아미드를 포함한다. 대표적인 예는 비제한적으로 호모폴리아미드, 예컨대 폴리아미드 6, 폴리아미드 66, 폴리아미드 56, 폴리아미드 46, 폴리아미드 4T, 폴리아미드 5T, 폴리아미드 6T, 폴리아미드 6I, 폴리아미드 7T, 폴리아미드 8T, 폴리아미드 9T, 폴리아미드 10T, 폴리아미드 11T, 폴리아미드 12T, 폴리아미드 MXD6, 및 이의 코폴리아미드를 포함하고; 더욱 바람직하게는 열가소성 매트릭스 수지는 265℃ 초과 온도로 녹는 폴리아미드, 예컨대 폴리아미드 4T, 폴리아미드 5T, 폴리아미드 6T, 폴리아미드 6I, 폴리아미드 7T, 폴리아미드 8T, 폴리아미드 9T, 폴리아미드 10T, 폴리아미드 11T, 폴리아미드 12T, 폴리아미드 MXD6, 및 이의 코폴리아미드 및/또는 폴리아미드 4T, 폴리아미드 5T, 폴리아미드 6T, 폴리아미드 6I, 폴리아미드 7T, 폴리아미드 8T, 폴리아미드 9T, 폴리아미드 10T, 폴리아미드 11T, 폴리아미드 12T, 또는 폴리아미드 6, 폴리아미드 66, 폴리아미드 56 및 폴리아미드 46으로부터 선택된 하나 이상과 공중합된 폴리아미드 MXD6 중 하나 이상의 공중합체; 예컨대 폴리아미드 6/6T, 폴리아미드 6I/6T, 폴리아미드 6/10T, 폴리아미드 66/6T, 폴리아미드 46/4T, 폴리아미드 10T/6T, 폴리아미드 6T/5T, 폴리아미드 6T/10T, 폴리아미드 66/4T/46[이는 폴리아미드 66, 폴리아미드 4T 및 폴리아미드 46의 코폴리아미드이다], 폴리아미드 6T/4T/46[이는 폴리아미드 6T, 폴리아미드 4T 및 폴리아미드 46의 코폴리아미드이다], 폴리아미드 6T/66/46[폴리아미드 6T, 폴리아미드 66 및 폴리아미드 46의 코폴리아미드], 폴리아미드 6T/5T/56[폴리아미드 6T, 폴리아미드 5T 및 폴리아미드 56의 코폴리아미드] 및 폴리아미드 6T/66/56[폴리아미드 6T, 폴리아미드 66 및 폴리아미드 56의 코폴리아미드]이고; 가장 바람직하게는, 열가소성 매트릭스 수지는 폴리아미드 66/4T/46, 폴리아미드 6T/4T/46, 폴리아미드 6T/66/46, 폴리아미드 6T/5T/56 및 폴리아미드 6T/66/56이고; 더욱더 바람직하게는, 열가소성 매트릭스 수지는 폴리아미드 66/4T/46, 예컨대 스타닐 포르티(Stanyl ForTii: 상표) DS100이다.Preferably, the thermoplastic matrix resin comprises a polyamide. Representative examples include, but are not limited to, homopolyamides such as polyamide 6, polyamide 66, polyamide 56, polyamide 46, polyamide 4T, polyamide 5T, polyamide 6T, polyamide 6I, polyamide 7T, polyamide 8T , Polyamide 9T, polyamide 10T, polyamide 11T, polyamide 12T, polyamide MXD6, and copolyamides thereof; More preferably, the thermoplastic matrix resin is a polyamide which melts at above 265 DEG C, such as polyamide 4T, polyamide 5T, polyamide 6T, polyamide 6I, polyamide 7T, polyamide 8T, polyamide 9T, polyamide 10T, Polyamide 11T, polyamide 12T, polyamide MXD6, and copolyamide and / or polyamide 4T thereof, polyamide 5T, polyamide 6T, polyamide 6I, polyamide 7T, polyamide 8T, polyamide 9T, 10T, polyamide 11T, polyamide 12T, or polyamide MXD6 copolymerized with at least one selected from polyamide 6, polyamide 66, polyamide 56 and polyamide 46; Polyamide 6T / 10T, polyamide 6T / 10T, polyamide 6 / 6T, polyamide 6 / 6T, polyamide 6 / 6T, polyamide 6 / 10T, polyamide 66 / 6T, polyamide 46 / 4T, Amide 66 / 4T / 46 [which is a copolyamide of polyamide 66, polyamide 4T and polyamide 46], polyamide 6T / 4T / 46 [which is a polyamide 6T, a polyamide 4T and a polyamide 46 copolyamide , Polyamide 6T / 66/46 [copolyamide of polyamide 6T, polyamide 66 and polyamide 46], polyamide 6T / 5T / 56 [polyamide 6T, polyamide 5T and copolyamide of polyamide 56 Amide] and polyamide 6T / 66/56 [copolyamide of polyamide 6T, polyamide 66 and polyamide 56]; Most preferably, the thermoplastic matrix resin is a polyamide 66 / 4T / 46, a polyamide 6T / 4T / 46, a polyamide 6T / 66/46, a polyamide 6T / 5T / 56 and a polyamide 6T / 66/56; Even more preferably, the thermoplastic matrix resin is a polyamide 66 / 4T / 46, such as Stanyl ForTii (trademark) DS100.

본 발명의 조성물에 존재하는 열가소성 매트릭스 수지의 양은 조성물의 선택된 특성뿐만 아니라 이러한 조성물로부터 제조된 성형 물품에 기초한다. 인자는 사용된 LDS 첨가제의 유형 및/또는 양을 포함한다.The amount of thermoplastic matrix resin present in the composition of the present invention is based on the selected properties of the composition as well as the shaped article made from such a composition. Factors include the type and / or amount of LDS additive used.

바람직하게는, 열가소성 매트릭스 수지는 42.5 중량% 내지 94 중량%, 더욱 바람직하게는 50 중량% 내지 80 중량%, 가장 바람직하게는 65 중량% 내지 75 중량%의 양으로 존재한다.Preferably, the thermoplastic matrix resin is present in an amount of from 42.5 wt% to 94 wt%, more preferably from 50 wt% to 80 wt%, and most preferably from 65 wt% to 75 wt%.

열가소성 매트릭스 수지는 섬유 보강제를 첨가하여 강화될 수 있다. 임의의 적합한 섬유 보강제, 예컨대 유리 섬유, 탄소 섬유, 현무암 섬유 또는 아라미드 섬유가 본 발명에 사용될 수 있다. 섬유 보강제는 5 중량% 내지 50 중량%, 바람직하게는 15 중량% 내지 35 중량%, 더욱 바람직하게는 20 중량% 내지 30 중량%, 가장 바람직하게는 약 30 중량%로 존재한다.The thermoplastic matrix resin may be reinforced by the addition of a fiber reinforcing agent. Any suitable fiber reinforcement, such as glass fiber, carbon fiber, basalt fiber or aramid fiber, may be used in the present invention. The fiber reinforcement is present in an amount of from 5% to 50% by weight, preferably from 15% to 35% by weight, more preferably from 20% to 30% by weight, most preferably about 30% by weight.

열가소성 매트릭스 수지 이외에, 본 발명의 조성물은 또한 레이저 직접 구조화(LDS) 첨가제를 포함한다. LDS 첨가제는, 조성물이 LDS 방법에 사용될 수 있도록 선택된다. LDS 방법에서, LDS 첨가제를 조성물의 표면에 놓고 LDS 첨가제로부터 금속 원자를 활성화하기 위해 레이저 빔에 노출시킨다. 상기와 같이, LDS 첨가제는 레이저 빔에 노출될 때 금속 원자가 활성화되고, 레이저 빔에 노출되지 않은 영역에서 금속 원자가 노출되지 않도록 선택된다. 또한, LDS 첨가제는 레이저 빔에 노출된 후 에칭 영역이 구리 도금 공정과 같은 표준 무전해 도금 공정에 따라 전도성 경로를 형성하기 위해 도금될 수 있도록 선택된다. 사용될 수 있는 다른 무전해 도금 공정은 비제한적으로 금 도금, 니켈 도금, 은 도금, 아연 도금, 주석 도금 등을 포함한다.In addition to thermoplastic matrix resins, the compositions of the present invention also include laser direct structured (LDS) additives. The LDS additive is selected so that the composition can be used in the LDS method. In the LDS method, an LDS additive is placed on the surface of the composition and exposed to a laser beam to activate metal atoms from the LDS additive. As described above, the LDS additive is selected such that the metal atoms are activated when exposed to the laser beam and are not exposed to the metal atoms in the areas not exposed to the laser beam. In addition, the LDS additive is selected so that the etched region after being exposed to the laser beam can be plated to form a conductive path in accordance with a standard electroless plating process, such as a copper plating process. Other electroless plating processes that may be used include, but are not limited to, gold plating, nickel plating, silver plating, galvanizing, tin plating, and the like.

LDS 첨가제를 사용하는 목적은 하기 도금 공정 동안 레이저 에칭된 표면 및 최종 금속화 층상에 금속 시드를 형성하는 것이다.The purpose of using the LDS additive is to form a metal seed on the laser etched surface and the final metallization layer during the subsequent plating process.

존재하는 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서 x는 0.60 초과 및 0.85 미만이다. ZnXNi(1-x)Fe2O4는 스피넬 구조를 갖는 니텔-아연 페라이트의 한 종류이다. 이는 ZnFe2O4 및 NiFe2O4의 단순 혼합물이 아니다. 또한, 이는 일부 문헌에서 ZnFe2O4로 도핑된 NiFe2O4로 기재된다. 이 출원과 관련하여, ZnXNi(1-x)Fe2O4는 또한 니켈-아연 페라이트 중 Zn 및 Ni의 몰비로 나타낼 수 있다. 예를 들면, Zn0 . 75Ni0 . 25Fe2O4는 75Zn/25Ni로 나타낼 수 있다. Zn Fe2O4는 100Zn로 나타낼 수 있고, Ni Fe2O4는 100Ni로 나타낼 수 있다. Existing laser direct structured additives are represented by the formula Zn x Ni (1-x) Fe 2 O 4 , where x is greater than 0.60 and less than 0.85. Zn X Ni (1-x) Fe 2 O 4 is a kind of nickel-zinc ferrite having a spinel structure. This is not a simple mixture of ZnFe 2 O 4 and NiFe 2 O 4 . Also, This is described in some documents as NiFe 2 O 4 doped with ZnFe 2 O 4 . In connection with this application, Zn X Ni (1-x) Fe 2 O 4 can also be expressed as the molar ratio of Zn and Ni in the nickel-zinc ferrite. For example, Zn 0 . 75 Ni 0 . 25 Fe 2 O 4 can be represented by 75Zn / 25Ni. Zn Fe 2 O 4 can be represented by 100 Zn, and Ni Fe 2 O 4 can be represented by 100 Ni.

바람직하게는, X 값은 0.65 초과 및 0.80 미만; 더욱 바람직하게는 0.70 초과 및 0.75 미만이고; 가장 바람직하게는, X 값은 0.75이고 레이저 구조화 첨가제는 Zn0.75Ni0.25Fe2O4이다.Preferably, the X value is greater than 0.65 and less than 0.80; More preferably greater than 0.70 and less than 0.75; Most preferably, the X value is 0.75 and the laser structuring additive is Zn 0.75 Ni 0.25 Fe 2 O 4 .

포함된 LDS 첨가제의 양은 기계적 특성에 나쁜 영향을 끼치지 않으면서 레이저에 의해 활성화 후 형성된 전도성 경로를 도금하기에 충분하다. 일 예에서, LDS 첨가제는 1 중량% 내지 7.5 중량%, 바람직하게는 2.5 중량% 내지 6 중량%, 더욱 바람직하게는 3 중량% 내지 5 중량%, 가장 바람직하게는 5 중량%의 양으로 존재한다. 일반적으로, 레이저 직접 구조화 첨가제가 많이 존재할수록, 수득되는 도금 품질은 더욱 좋다. 레이저 구조화 첨가제의 양이 7.5 중량%를 초과할 때, 물질의 기계적 성능은 불리할 것이다.The amount of LDS additive included is sufficient to coat the conductive path formed after activation by the laser without adversely affecting the mechanical properties. In one example, the LDS additive is present in an amount of 1 wt% to 7.5 wt%, preferably 2.5 wt% to 6 wt%, more preferably 3 wt% to 5 wt%, and most preferably 5 wt% . In general, the greater the number of laser direct structured additives present, the better the resulting plating quality. When the amount of the laser structuring additive exceeds 7.5% by weight, the mechanical performance of the material will be disadvantageous.

레이저 구조화 첨가제의 입자 크기 분산은 적합하게는 50 nm 내지 50 ㎛, 바람직하게는, 100 nm 내지 10 ㎛, 더욱 바람직하게는 0.5 ㎛ 내지 3 ㎛이다.The particle size dispersion of the laser structured additive is suitably 50 nm to 50 mu m, preferably 100 nm to 10 mu m, more preferably 0.5 mu m to 3 mu m.

바람직하게는, 열가소성 조성물은 조성물의 총 중량을 기준으로Preferably, the thermoplastic composition comprises, based on the total weight of the composition

d) 0 내지 30 중량%의 난연제;d) from 0 to 30% by weight of a flame retardant;

e) 0 내지 20 중량%의 기타 첨가제e) 0 to 20% by weight of other additives

를 추가로 포함한다..

당업자에게 널리 공지된 임의의 난연제가 본 발명에서 사용될 수 있다. 바람직하게는 난연제는 비제한적으로 금속 하이드록사이드, 예컨대 알루미늄 하이드록사이드 및 마그네슘 하이드록사이드, 질소계 난연제, 예컨대 멜라민 및 멜라민 유도체, 인계 난연제, 예컨대 유기 및 무기 포스페이트, 포스포네이트, 포스피네이트, 예를 들면 금속 포스피네이트, 및 적린으로부터 선택된 하나 이상; 바람직하게는 인계 난연제, 질소계 난연제 및 인계 난연제의 배합물; 더욱 바람직하게는 금속 포스피네이트를 포함한다.Any of the flame retardants well known to those skilled in the art may be used in the present invention. Preferably, the flame retardant is selected from, but not limited to, metal hydroxides such as aluminum hydroxide and magnesium hydroxide, nitrogen based flame retardants such as melamine and melamine derivatives, phosphorus flame retardants such as organic and inorganic phosphates, phosphonates, phosphinates , E.g., metal phosphinate, and acyl; A combination of a phosphorus-based flame retardant, a nitrogen-based flame retardant and a phosphorus-based flame retardant; More preferably a metal phosphinate.

난연제는, 난연제가 조성물에 첨가되기 전에 당업자에 널리 공지된 임의의 방법에 의해 변형될 수 있다.The flame retardant may be modified by any method well known to those skilled in the art before the flame retardant is added to the composition.

성분 d)의 난연제는 적합하게는 0 중량% 내지 30 중량%, 바람직하게는 10 중량% 내지 30 중량%로 존재한다.The flame retardant of component d) is suitably present from 0% to 30% by weight, preferably from 10% to 30% by weight.

성분 e)의 첨가제는 당업자에게 널리 공지된 임의의 보조제, 예컨대 안료, 산화방지제, 광 안정화제, 열 안정화제, 정전기 방지제, 자외선(UV) 흡수제, 이형제, 윤활제, 발포제 또는 조성물에 첨가될 수 있는 다른 특성을 개선하기에 적합한 기타 충전제일 수 있다.The additives of component e) can be added to any of the additives well known to those skilled in the art such as pigments, antioxidants, light stabilizers, heat stabilizers, antistatic agents, UV absorbers, release agents, lubricants, Other fillers may be suitable for improving other properties.

성분 e)의 첨가제는 적합하게는 0 중량% 내지 20 중량%, 바람직하게는 0.5 중량% 내지 5 중량%로 존재한다.The additive of component e) suitably is present from 0% to 20% by weight, preferably from 0.5% to 5% by weight.

또한, 본원은In addition,

활성화된 패턴을 갖는 성형 물품;A molded article having an activated pattern;

상기 활성화된 패턴에 도금되어 전도성 경로를 형성하는 구리 층A copper layer plated on the activated pattern to form a conductive path

을 포함하는 제품을 또한 제공하고,Lt; RTI ID = 0.0 > a < / RTI &

상기 성형 물품은The molded article

a) 42.5 중량% 내지 94 중량%의 열가소성 매트릭스 수지;a) from 42.5% to 94% by weight of a thermoplastic matrix resin;

b) 1 중량% 내지 7.5 중량%의 레이저 직접 구조화 첨가제; 및b) from 1% to 7.5% by weight of a laser direct structured additive; And

c) 5 중량% 내지 50 중량%의 섬유 보강제c) 5% to 50% by weight of fiber reinforcement

를 포함하고 레이저를 사용하여 활성화된 후 도금될 수 있는 열가소성 조성물로부터 형성되고;≪ / RTI > is formed from a thermoplastic composition that can be plated after activation using a laser;

상기 중량%는 조성물의 총 중량을 기준으로 하고;Said weight percent being based on the total weight of the composition;

상기 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서, x는 0.60 초과 및 0.85 미만이다.The laser direct structured additive is represented by the formula Zn x Ni (1-x) Fe 2 O 4 , where x is greater than 0.60 and less than 0.85.

본원에 개시된 물품은 의학, 자동차, 항공우주, 군대, RF 안테나, 센서, 주택 보안 및 커넥터의 분야에서 사용될 수 있다.The articles disclosed herein may be used in the fields of medicine, automotive, aerospace, military, RF antennas, sensors, home security and connectors.

또한, 본원은 In addition,

열가소성 조성물로부터 물품을 성형하는 단계;Molding the article from the thermoplastic composition;

레이저를 사용하여 상기 성형 물품에 활성화된 패턴을 형성하는 단계; 및Forming an activated pattern on the shaped article using a laser; And

구리 층을 상기 활성화된 패턴 위에 도금하여 전도성 경로를 형성하는 단계Plating a copper layer over the activated pattern to form a conductive path

를 포함하는 제품의 형성 방법을 제공하고,The method comprising the steps of:

상기 열가소성 조성물은 조성물의 총 중량을 기준으로The thermoplastic composition may comprise, based on the total weight of the composition,

a) 42.5 중량% 내지 94 중량%의 열가소성 매트릭스 수지;a) from 42.5% to 94% by weight of a thermoplastic matrix resin;

b) 1 중량% 내지 7.5 중량%의 레이저 직접 구조화 첨가제; 및b) from 1% to 7.5% by weight of a laser direct structured additive; And

c) 5 중량% 내지 50 중량%의 섬유 보강제c) 5% to 50% by weight of fiber reinforcement

를 포함하고 레이저를 사용하여 활성화된 후 도금될 수 있고;≪ / RTI > and may be activated using a laser and then plated;

상기 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서, x는 0.60 초과 및 0.85 미만이다.The laser direct structured additive is represented by the formula Zn x Ni (1-x) Fe 2 O 4 , where x is greater than 0.60 and less than 0.85.

본 발명의 열가소성 조성물은 다중 성분을 조합하여 수지를 형성하는 임의의 공지된 방법을 사용하여 형성될 수 있다. 일 실시양태에서, 성분을 먼저 고속 혼합기에서 또는 다른 저전단 공정으로 배합하였다. 이어서, 상기 배합물을 호퍼(hopper)를 통해 이축 압출기의 스로트(throat)에 공급하였다. 압출기는 일반적으로 조성물의 유동을 야기하기에 필요한 온도보다 높은 온도에서 작동한다.The thermoplastic compositions of the present invention can be formed using any known method of combining the multiple components to form a resin. In one embodiment, the components were first blended in a high-speed mixer or in another low shear process. The formulation was then fed through a hopper to the throat of a twin-screw extruder. The extruder generally operates at a temperature higher than the temperature required to cause the flow of the composition.

열가소성 수지가 매트릭스 수지로서 사용될 때, LDS 첨가제를 열가소성 수지 및/또는 다른 첨가제 및/또는 난연제와 압출기에서 합성하여 목적한 조성물을 수득하였다. When the thermoplastic resin is used as a matrix resin, the LDS additive is synthesized in an extruder with a thermoplastic resin and / or other additives and / or a flame retardant to obtain a desired composition.

제조되거나 형성되거나 성형된 물품, 예컨대 조성물이 또한 제공된다. 열가소성 조성물은 주입 성형, 추출, 회전 성형, 취입 성형 및 열형성과 같은 다양한 수단에 의해 유용한 성형 제품으로 성형되어 예를 들면 컴퓨터, 노트북 및 휴대용 컴퓨터용 하우징, 휴대폰 및 다른 상기 통신 장비용 하우징; 의료 적용, 자동차 적용 등의 부품과 같은 물품을 형성할 수 있다.Articles made, formed or molded, such as compositions, are also provided. Thermoplastic compositions can be formed into useful molded articles by a variety of means such as injection molding, extrusion, rotary molding, blow molding, and thermoforming, for example housings for computers, notebooks and portable computers, housings for mobile phones and other such communication equipment; Medical applications, automotive applications, and the like.

실시예Example

본 발명은 하기 실시예로 예시될 수 있지만 이로 제한되지 않는다.The present invention can be illustrated by the following examples, but is not limited thereto.

재료material

폴리아미드: 디에스엠(DSM)으로부터의 스타닐 포르티(상표) DS100.Polyamide: Stannyl Portey (trademark) DS100 from DSM.

LDS 첨가제:LDS additive:

- 셰퍼드 컬러 컴퍼니(Shepherd Color Company)로부터 시판중인 제품 셰퍼드 블랙(Shepherd Black) 1G(CuCr2O4)Shepherd Black 1G (CuCr 2 O 4 ), a product commercially available from the Shepherd Color Company,

- 네오시드 페메트라이더 게엠베하 안트 컴퍼니(Neosid Pemetzrieder GmbH & Co)로부터 시판중인 제품 시리즈 네오F20FERPO[75Ni/25Zn]: 네오F2FERPO[50Ni/50Zn]; 네오MIX25Ni75Zn[25Ni/75Zn]; 네오MIX100Zn[100Zn]; 네오F100[100Ni].Product series Neo F20FERPO [75Ni / 25Zn]: Neo F2FERPO [50Ni / 50Zn] commercially available from Neosid Pemetzrieder GmbH &Co; Neo MIX25Ni75Zn [25Ni / 75Zn]; Neo MIX100Zn [100Zn]; Neo F100 [100Ni].

유리 섬유: 피피지 인더스트리즈 인코포레이티드(PPG Industries Inc.)로부터의 표준 유리 단섬유 - CIPC 3014B. Glass fiber: Standard glass short fibers from PPG Industries Inc. - CIPC 3014B.

도금 욕 조성물: 엔톤 게엠베하(Enthone GmbH)로부터 직접 수득가능한 엔플레이트(ENPLATE: 등록상표) 케미칼 용액.Plating bath composition: Enplate (TM) chemical solution obtainable directly from Enthone GmbH.

실시예 1Example 1

65 중량%의 스타닐 포르티(상표) DS100, 30 중량%의 유리 섬유 및 5 중량%의 첨가제를 표준 DSM 스타닐 포르티(상표) 혼합 조건에 따라 크라우스마페이 베르스토르프(KrausMaffei Berstorff)로부터 ZE25 이축 압출기에서 혼합하였다. 압출 후, 수득된 혼합 물질을 사출 성형을 위해 과립으로 절단하였다. 사출 성형 과정에서, 이러한 과립은 80 x 80 x 2 mm 크기의 플라크를 형성하였다. 이어서, 사출 성형 플라크를 표 1에 나타낸 하기 파라미터 설정으로 트럼프 레이저 마크 머신(Trumph Laser Mark Machine)에 넣었다. 사용된 레이저 유형은 1064 nm의 파장을 갖는 Nd:YAG 레이저이다.65 wt% Stanny Forti (TM) DS100, 30 wt% glass fibers, and 5 wt% additives were mixed with Kraus Maffei Berstorff according to standard DSM Stannol Forti (TM) Were mixed in a ZE25 twin-screw extruder. After extrusion, the obtained mixed material was cut into granules for injection molding. During the injection molding process, these granules formed plaques measuring 80 x 80 x 2 mm. The injection-molded plaques were then placed in a Trumph Laser Mark Machine with the following parameter settings shown in Table 1: The type of laser used is an Nd: YAG laser with a wavelength of 1064 nm.

도금 욕의 온도를 48℃로 올리고 온도를 48℃에서 유지하였다. 레이저 처리 후, 레이저 처리된 플라크를 구리 무전해 도금 욕에 30 분 동안 완전히 함침시켰다. 도금 전 및 후, 플라크를 탈이온수로 세척하였다.The temperature of the plating bath was raised to 48 캜 and the temperature was maintained at 48 캜. After laser treatment, the laser treated plaques were thoroughly impregnated in a copper electroless plating bath for 30 minutes. Before and after plating, the plaques were washed with deionized water.

실시예 1에서 사용된 레이저 기기의 파라미터 설정 및 플라그 상에 도금된 구리 층의 도금 생성-두께를 표 1에 나타내었다.The parameter settings of the laser instrument used in Example 1 and the plated generation-thickness of the plated copper layer on the plagues are shown in Table 1.

펄스 주파수(kHz)
/레이저 파워
( 200W의 %)
Pulse frequency (kHz)
/ Laser power
(% Of 200 W)
60/7060/70 60/8060/80 60/9060/90 80/7080/70 80/8080/80 80/9080/90 100/70100/70 100/80100/80 100/90100/90
LDS 첨가제LDS Additive 100Ni100Ni 00 00 00 00 00 00 00 00 00 75Ni/25Zn75Ni / 25Zn 0.10.1 0.50.5 0.90.9 0.10.1 0.40.4 0.70.7 0.10.1 0.30.3 0.50.5 50Ni/50Zn50Ni / 50Zn 0.60.6 1.61.6 1.81.8 0.50.5 1.41.4 1.61.6 0.40.4 1One 1.41.4 25Ni/75Zn25Ni / 75Zn 0.80.8 3.13.1 3.63.6 0.90.9 2.22.2 3.53.5 0.90.9 22 3.33.3 100Zn100Zn 0.40.4 1.51.5 1.51.5 0.40.4 1.21.2 1.51.5 0.40.4 0.80.8 1.41.4 블랙 1G(CuCr2O4)Black 1G (CuCr 2 O 4 ) 2.82.8 6.16.1 6.46.4 2.32.3 5.25.2 5.85.8 22 3.83.8 5.15.1

결론conclusion

표 1로부터, 25Ni/75Zn LDS 첨가제를 포함하는 본 발명에 따른 조성물은 30분 이내에 도금될 수 있고, 생성된 구리 층 두께는 (CuCr2O4)를 포함하는 조성물의 두께보다 더 얇을지라도 100Ni, 75Ni/25Zn, 50Ni/50Zn 및 100Zn을 포함하는 조성물의 두께보다 더 두껍다는 것을 알 수 있다. From Table 1 it can be seen that the composition according to the invention comprising 25Ni / 75Zn LDS additive can be plated within 30 minutes and the resulting copper layer thickness is less than the thickness of the composition comprising (CuCr 2 O 4 ) Lt; RTI ID = 0.0 > 75Ni / 25Zn, 50Ni / 50Zn and 100Zn. ≪ / RTI >

실시예 2Example 2

기계적 특성Mechanical properties

65 중량%의 스타닐 포르티(상표) DS100, 30 중량%의 유리 섬유 및 5 중량%의 LDS 첨가제를 함유하는 과립을 인장 시험 ISO 527 및 샤르피 시험 ISO 179를 위한 표준 막대로 사출 성형하고, 결과를 하기 표 2에 나타내었다.Granules containing 65% by weight of Stannyl Porty (TM) DS100, 30% by weight of glass fibers and 5% by weight of LDS additives were injection molded into standard bars for tensile test ISO 527 and Charpy test ISO 179, Are shown in Table 2 below.

E-모듈러스E-modulus 인장 강도The tensile strength 파단신율Elongation at break 샤르피 비노치Charpy Bianchi 샤르피 노치Charpinot MpaMpa MpaMpa %% kJ/M2kJ / M2 kJ/M2kJ / M2 [100Zn][100Zn] 1113811138 126.5126.5 1.261.26 30.7830.78 3.753.75 [25Ni/75Zn][25Ni / 75Zn] 1124011240 124.9124.9 1.241.24 29.3429.34 3.653.65 [50Ni/50Zn][50Ni / 50Zn] 1139311393 106.2106.2 1.041.04 29.1129.11 3.333.33 [75Ni/25Zn][75Ni / 25Zn] 1144411444 110.3110.3 1.081.08 29.0629.06 3.563.56 [100Ni][100Ni] 1122611226 106.3106.3 1.071.07 26.9126.91 3.043.04 블랙 1G(CuCr2O4)Black 1G (CuCr 2 O 4 ) 1122011220 110.6110.6 1.081.08 26.3226.32 3.413.41

결론conclusion

상기 표 2에 나타낸 데이터에 따라, CuCr2O4를 포함하는 조성물과 Ni 및/또는 Zn 페라이트를 포함하는 다른 조성물을 비교하면, 25Ni/75Zn을 포함하는 조성물의 기계적 특성, 즉, 파단신율 및 강도는 잘 개선되었다.According to the data shown in Table 2 above, comparing compositions comprising CuCr 2 O 4 with other compositions comprising Ni and / or Zn ferrite, the mechanical properties of compositions comprising 25Ni / 75Zn, ie, elongation at break and strength Was improved.

Claims (14)

(a) 42.5 중량% 내지 94 중량%의 열가소성 매트릭스 수지;
(b) 1 중량% 내지 7.5 중량%의 레이저 직접 구조화 첨가제; 및
(c) 5 중량% 내지 50 중량%의 섬유 보강제
를 포함하고 레이저를 사용하여 활성화된 후 도금될 수 있는 열가소성 조성물로서,
상기 중량%는 조성물의 총 중량을 기준으로 하고;
상기 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서 x는 0.60 초과 및 0.85 미만인, 열가소성 조성물.
(a) from 42.5% to 94% by weight of a thermoplastic matrix resin;
(b) 1% to 7.5% by weight of a laser direct structured additive; And
(c) 5% to 50% by weight of fiber reinforcement
A thermoplastic composition that can be activated after laser activation,
Said weight percent being based on the total weight of the composition;
Wherein the laser direct structured additive is represented by the formula Zn x Ni (1-x) Fe 2 O 4 , where x is greater than 0.60 and less than 0.85.
제 1 항에 있어서,
x가 0.65 내지 0.80인 열가소성 조성물.
The method according to claim 1,
x is from 0.65 to 0.80.
제 2 항에 있어서,
x가 0.70 내지 0.75, 바람직하게는 0.75이고; 레이저 직접 구조화 첨가제가 2.5 중량% 내지 6 중량%, 바람직하게는 3 중량% 내지 5 중량%, 더욱 바람직하게는 5 중량%의 양으로 존재하는, 열가소성 조성물.
3. The method of claim 2,
x is 0.70 to 0.75, preferably 0.75; Wherein the laser direct structured additive is present in an amount of 2.5 wt% to 6 wt%, preferably 3 wt% to 5 wt%, more preferably 5 wt%.
제 1 항 내지 제 3 항 중 어느 한 항에 있어서,
보강제가 유리 섬유, 탄소 섬유, 현무암 섬유 및 아라미드 섬유로부터 하나 이상 선택되고, 바람직하게는 유리 섬유인 열가소성 조성물.
4. The method according to any one of claims 1 to 3,
Wherein the reinforcing agent is at least one selected from glass fibers, carbon fibers, basalt fibers and aramid fibers, and is preferably glass fiber.
제 1 항 내지 제 4 항 중 어느 한 항에 있어서,
섬유 보강제가 10 중량% 내지 50 중량%, 바람직하게는 15 중량% 내지 35 중량%, 더욱 바람직하게는 20 중량% 내지 30 중량%의 양으로 존재하는 열가소성 조성물.
5. The method according to any one of claims 1 to 4,
Wherein the fiber reinforcing agent is present in an amount of from 10 wt% to 50 wt%, preferably from 15 wt% to 35 wt%, more preferably from 20 wt% to 30 wt%.
제 1 항 내지 제 5 항 중 어느 한 항에 있어서,
열가소성 수지가 폴리에스터, 폴리아미드, 폴리페닐렌 설파이드, 폴리페닐렌 옥사이드, 폴리설폰, 폴리아릴레이트, 폴리에테르에테르케톤 및 폴리에테르이미드, 및 이의 혼합물 및/또는 공중합체로 이루어진 군으로부터 하나 이상 선택되는 열가소성 조성물.
6. The method according to any one of claims 1 to 5,
Wherein the thermoplastic resin is at least one selected from the group consisting of polyesters, polyamides, polyphenylene sulfides, polyphenylene oxides, polysulfones, polyarylates, polyetheretherketones and polyetherimides, and mixtures and / or copolymers thereof Lt; / RTI >
제 1 항 내지 제 6 항 중 어느 한 항에 있어서,
열가소성 매트릭스 수지가 폴리아미드를 포함하는 열가소성 조성물.
7. The method according to any one of claims 1 to 6,
Wherein the thermoplastic matrix resin comprises a polyamide.
제 1 항 내지 제 7 항 중 어느 한 항에 있어서,
금속 하이드록사이드, 질소계 난연제 및 인계 난연제로부터 선택된 하나 이상의 난연제를 포함하는 열가소성 조성물.
8. The method according to any one of claims 1 to 7,
Wherein the thermoplastic composition comprises at least one flame retardant selected from the group consisting of metal hydroxides, nitrogen-based flame retardants, and phosphorus flame retardants.
제 1 항 내지 제 8 항 중 어느 한 항에 있어서,
조성물의 총 중량을 기준으로,
(d) 0 내지 30 중량%의 난연제; 및/또는
(e) 0 내지 20 중량%의 기타 첨가제
를 포함하는 열가소성 조성물.
9. The method according to any one of claims 1 to 8,
Based on the total weight of the composition,
(d) 0 to 30% by weight of a flame retardant; And / or
(e) 0 to 20% by weight of other additives
≪ / RTI >
제 9 항에 있어서,
난연제가 금속 하이드록사이드, 질소계 난연제 및 인계 난연제로부터 하나 이상 선택되는 열가소성 조성물.
10. The method of claim 9,
Wherein the flame retardant is selected from the group consisting of metal hydroxides, nitrogen flame retardants and phosphorus flame retardants.
활성화된 패턴을 갖는 성형 물품;
활성화된 패턴 상에 도금되어 전도성 경로를 형성하는 구리 층
을 포함하는 제품으로서,
상기 성형 물품은
(a) 42.5 중량% 내지 94 중량%의 열가소성 매트릭스 수지;
(b) 1 중량% 내지 7.5 중량%의 레이저 직접 구조화 첨가제; 및
(c) 5 중량% 내지 50 중량%의 섬유 보강제
를 포함하고 레이저를 사용하여 활성화된 후 도금될 수 있는 열가소성 조성물로부터 형성되고;
상기 중량%는 조성물의 총 중량을 기준으로 하고;
상기 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서 x는 0.60 초과 및 0.85 미만인, 제품.
A molded article having an activated pattern;
The copper layer plated on the activated pattern to form a conductive path
≪ / RTI >
The molded article
(a) from 42.5% to 94% by weight of a thermoplastic matrix resin;
(b) 1% to 7.5% by weight of a laser direct structured additive; And
(c) 5% to 50% by weight of fiber reinforcement
≪ / RTI > is formed from a thermoplastic composition that can be plated after activation using a laser;
Said weight percent being based on the total weight of the composition;
Wherein the laser direct structured additive is represented by the formula Zn x Ni (1-x) Fe 2 O 4 , where x is greater than 0.60 and less than 0.85.
제 11 항에 있어서,
열가소성 조성물이 제 1 항 내지 제 10 항 중 어느 한 항에 정의된 조성물인 제품.
12. The method of claim 11,
Wherein the thermoplastic composition is a composition as defined in any one of claims 1 to 10.
열가소성 조성물로부터 물품을 성형하는 단계;
레이저를 사용하여 상기 성형 물품상에 활성화된 패턴을 형성하는 단계; 및
상기 활성화된 패턴상에 구리 층을 도금하여 전도성 경로를 형성하는 단계
를 포함하는 제품의 형성 방법으로서,
상기 열가소성 조성물은 조성물의 총 중량을 기준으로
a) 42.5 중량% 내지 94 중량%의 매트릭스 수지;
b) 1 중량% 내지 7.5 중량%의 레이저 직접 구조화 첨가제; 및
c) 5 중량% 내지 50 중량%의 섬유 보강제
를 포함하고 레이저를 사용하여 활성화된 후 도금될 수 있고,
상기 레이저 직접 구조화 첨가제는 화학식 ZnXNi(1-x)Fe2O4로 표시되되, 여기서 x는 0.60 초과 및 0.85 미만인, 방법.
Molding the article from the thermoplastic composition;
Forming an activated pattern on the shaped article using a laser; And
Plating the copper layer on the activated pattern to form a conductive path
1. A method of forming a product comprising:
The thermoplastic composition may comprise, based on the total weight of the composition,
a) from 42.5% to 94% by weight of a matrix resin;
b) from 1% to 7.5% by weight of a laser direct structured additive; And
c) 5% to 50% by weight of fiber reinforcement
Lt; / RTI > and may be activated using a laser and then plated,
Wherein the laser direct structured additive is represented by the formula Zn x Ni (1-x) Fe 2 O 4 , wherein x is greater than 0.60 and less than 0.85.
제 11 항에 있어서,
열가소성 조성물이 제 1 항 내지 제 10 항 중 어느 한 항에 정의된 조성물인 방법.
12. The method of claim 11,
Wherein the thermoplastic composition is a composition as defined in any one of claims 1 to 10.
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US20170107348A1 (en) 2017-04-20
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